Aluminium Alloy 7050 Chemical Composition Properties, Grades, Chart and Pdf
Aluminium Alloy 7050 is a strong type of material frequently utilized in aircraft operations because of its extraordinary mechanical characteristics. Aluminum is the main component with other essential parts including zinc as the alloying element and then copper as well as magnesium in smaller proportions. This alloy performs very well in terms of strength, light weight, corrosion resistance, and machinability, which allows its utilisation in the most essential structural parts of planes, and other high technology industries. It has top-notch chemical fingerprint that expose different fabrication techniques necessary for the purpose of molding. Acting as design reasons, grade of 7050 alloys and its forms are commonly used in structural applications, where strength and strength are essential. The complete charts and innovated PDFs, which allows the engineers and manufacturers to be able to pick the right alloy for the required case, helps them in the selection of the best alloy.
Aluminium Alloy 7050 Chemical Composition And Grade Table
Aluminum Alloy 7050 is a universal material with high strength, which is often found in aerospace and structural applications. The chemical composition of this metal is generally such that it contains 87.6% aluminium, 2.5% copper, 2.3% magnesium, and 5.6% zinc. Additionally, it may also involve other elements like silicon, iron, manganese, and titanium at the level of 1.6%. With its high strength-to-weight ratio, and the resistance to corrosion, this alloy is a perfect choice for space motors. Another important prerogative of purpose steel is that it can be heat-treated to further improve its mechanical properties. Alloy 7050 provides strength, toughness, and high fatigue resistance as the components of important aircraft structures, missile parts, and high-performance sporting goods.
| Elements | Aluminum, Al | Copper, Cu | Magnesium, Mg | Zinc, Zn | Zirconium, Zr |
|---|---|---|---|---|---|
| Min (%) | - | - | - | - | - |
| Max (%) | 89 | 2.3 | 2.3 | 6.2 | 0.12 |
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